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22001100 in conjunction with

TThhee 5500tthh JJSSAASSSS CCoonnffeerreennccee oonn AAeerroossppaaccee PPrrooppuullssiioonn aanndd PPoowweerr March 4-6, 2010

Miyazaki Kanko Hotel, Miyazaki, Japan Organized by

The Japan Society for Aeronautical and Space Sciences (JSASS) Co-organized by

The Korean Society of Propulsion Engineers (KSPE) The Chinese Society of Engineering Thermophysics (CSET)

Collaborated by Gas Turbine Society of Japan (GTSJ) The Japan Society of Mechanical Engineers (JSME) Japan Aeronautical Engineers' Association (JAEA)

AJCPP2010 International Organizing Committee

JAPAN

Prof. Toshinori Watanabe University of Tokyo (UT), AJCPP2010 Chairperson

Prof. Toshio Nagashima University of Tokyo (UT)

Prof. Takehiro Himeno University of Tokyo (UT), AJCPP2010 Secretary in General

KOREA

Prof. Chang Duk Kong Chosun University

Prof. In-Seuck Jeung Seoul National University (SNU)

Dr. Dae Sung Lee Korea Aerospace Research Institute (KARI)

CHINA

Prof. Xu Jianzhong Chinese Society of Engineering Thermophysics(CSET)

Prof. Xin Yuan Tsinghua Universit

Prof. Guang Xi Xi’an Jiaotong University

AJCPP2010 Local Organizing Committee

JAPAN

Prof. Toshinori Watanabe University of Tokyo (UT), Chairperson

Prof. Takehiro Himeno University of Tokyo (UT), Secretary

Mr. Hiroshi Kato Kawasaki Heavy Industries, Ltd. (KHI)

Dr. Kiyoshi Kinefuchi JAXA/Space Transportation Mission Directorate

Ms. Chiyuki Nakamata IHI Corporation

Prof. Kazutaka Nishiyama JAXA/Institute of Space and Astronautical Science

Mr. Mitsumasa Makida JAXA/Aviation Program Group

Mr. Jun Yabana Mitsubishi Heavy Industries, Ltd. (MHI)

Mr. Kengo Yamamoto IHI Aerospace, Co. Ltd. (IA)

KOREA

AJCPP2010 Secretary in Korea

Prof. Young-Bin Yoon Seoul National University (SNU)

CHINA

AJCPP2010 Secretary in China

Ms. Hongying Ke Chinese Society of Engineering Thermophysics (CSET)

AJCPP2010 General Information

Registration Registration Desk, 2nd floor, Miyazaki Kanko Hotel

0800-1700, March 4 (Thursday)

0800-1700, March 5 (Friday)

0800-1100, March 6 (Saturday)

Keynote Speeches Special Session Room, 3rd floor, Miyazaki Kanko Hotel

(1) ”HTV First Mission Results and Future Plan”

by Mr. Hiroshi Sasaki (Function Manager, HTV project team, JAXA)

1100 -1150, March 4 (Thursday)

(2) ”Current Korean Activities on Research and Development

of Air-Breathing Propulsion Systems”

by Prof. Changduk Kong (Dept. of Aerospace Engineering, Chosun University)

1700 - 1750, March 5 (Friday)

(3) ” Commercial Aviation Propulsion for the 21st Century”

by Dr. Alan H. Epstein (Vice President, Technology and Environment, Pratt & Whitney)

0820 -0910, March 6 (Saturday)

(4) ”Fundamental Studies on Performance Improvement of Scramjet Engine”

by Prof. Xinyu Chang (Institute of Mechanics, Chinese Academy of Sciences)

0910 -1000, March 6 (Saturday)

Buffet Lunch Buffet Restaurant, 3rd floor, Miyazaki Kanko Hotel

1200 - 1300, March 4 (Thursday)

1200 - 1300, March 5 (Friday)

Thursday and Friday lunches are served free for AJCPP2010 attendees.

Banquet Event Hall, 3rd floor, Miyazaki Kanko Hotel

1830 - 2030, March 5 (Friday)

Ticket for Friday Banquet is sold at Registration Desk (5000 JPY/Person).

Post-congress Tour Entrance, 1st floor, Miyazaki Kanko Hotel

1300 - 1800, March 6 (Saturday)

Tour Ticket is sold at Registration Desk (4000 JPY/Person), if seats are available.

Thursday Morning -March 4, 2010 AJCPP2010 in Miyazaki

Asian Joint Conference on

P P 2010Asian Joint Conference on

Propulsion and Power 2010March 3-6, 2010

Mi ki K k H t l Mi ki J

Thursday Morning -March 4, 2010

Session Room A2nd Floor “Hyuga”

Session Room B2nd Floor “Kurenai”


Propulsion and Power 2010

Time Table

March 3-6, 2010

Miyazaki Kanko Hotel, Miyazaki, Japan

2nd Floor Hyuga 2nd Floor Kurenai

Time A1. Numerical Simulation for Liquid Rocket Propulsion 1

Chae Hoon Sohn (Sejong University)Nobuyuki Tsuboi (Kyushu Institute of Technology)

B1.Axial Flow Turbine and Compressor 1 Yoshitaka Fukuyama (JAXA)Kuisoon Kim (Pusan National University)

0820 [AJCPP2010-015]Controlling the Secondary flows near Endwall Boundary Layer Fences in a 90° Turning Ductusing Approximate Optimization MethodJongjae Cho, Kuisoon Kim (Pusan National University, Busan)

0840 [AJCPP2010-146]Oscillatory Combustion inside a Model Combustion Chamber at Atmospheric ConditionTaro Shimizu, Dan Hori, Seiji Yoshida, Shigeru Tachibana, Shingo Matsuyama, Junji Shinjo,Yasuhiro Mizobuchi, Kan Kobayashi (JAXA)

[AJCPP2010-150]Numerical Investigations on Leakage Flow and Heat Transfer Characteristics of SquealerTip under Stator/Rotor InteractionJ. Li, J.S. Wang, Z.P. Feng (Xi’an Jiaotong University)

0900 [AJCPP2010 024] [AJCPP2010 025]0900 [AJCPP2010-024]A Numerical Study on Resonator Tuning in a Model Combustion ChamberJu Hyun Park, I Sun Park, Chae Hoon Sohn (Sejong University)

[AJCPP2010-025]Effects of Suction Surface Bump on Turbine Convergent-Divergent Rotor AerodynamicPerformanceLuo Weiwei, Zhang Lei, Wang Huishe, Xu Jianzhong, Huang Jiahua (Chinese Academy ofSciences)

0920 [AJCPP2010-153]Estimation of Thermodynamic Properties of Hydrogen, Oxygen and their Mixtures based onInter-molecular Interactions for Rocket Engine Combustion Flow AnalysisMitsuo Koshi, Kazuya Shimizu (University of Tokyo), Shin-ichi Tsuda (JAXA)

[AJCPP2010-002]Numerical Investigation on a New Type of Fully Reversible Axial Fan with Two Blade Rowson Both Sides of the RotorJingyin Li, Guang Xi, Penghua Guo, Weiwei Chen (Xi’an Jiaotong University)

0940 [AJCPP2010-151]Development of Efficient and Stable Time Integration Method for Detailed ChemicalKinetics by using Rate-Controlled Constrained Equilibrium (RCCE) Concept

[AJCPP2010-004]Aerodynamic design and preliminary analysis of a counter-rotating turbineQiao Jia-Fei, Zhao Qing-Jun, Xu Jian-Zhong (Chinese Academy of Sciences)Kinetics by using Rate-Controlled Constrained Equilibrium (RCCE) Concept

Mitsuo Koshi, Kazuya Shimizu (University of Tokyo)Qiao Jia-Fei, Zhao Qing-Jun, Xu Jian-Zhong (Chinese Academy of Sciences)

1000 [AJCPP2010-089]Construction of a reliable reduced CH4/O2 chemical reaction model under high pressurestatesYouhi Morii (The Graduate University for Advanced Studies), Nobuyuki Tsuboi (KyushuInstitute of Technology), Mitsuo Koshi (University of Tokyo), Hiroyuki Ogawa (JAXA), A.Koichi Hayashi (Aoyama Gakuin University), Taro Shimizu (JAXA)

1020 [AJCPP2010-084]MDRG Method for Kinetics Mechanism Simplification in Methane/Air Autoignition under GasTurbine ConditionSajjad Yousefian, Shahrokh Sorkhkhah (MAPNA Turbine Engineering and Manufacturing

[AJCPP2010-165]Film Cooling Effectiveness on a Rotating TurbineLi G., Deng H., Xiao J. (Beijing University of Aeronautics and Astronautics)

Company (TUGA)), Akbar Ghafourian, Masoud Darbandi (Sharif University of Technology)

1040

Keynote Speech 1Toshinori Watanabe (University of Tokyo)

Special Session Room3rd Floor “Hiyou”

1100 [AJCPP2010-S01]HTV First Mission Results and Future PlanHiroshi Sasaki (JAXA)

Coffee Break

Hiroshi Sasaki (JAXA)

1200 Lunch Buffet Restaurant (Free for AJCPP2010 attendees)3rd Floor “Hekisui”

1300Lunch Break


Propulsion and Power 2010

Time Table

March 3-6, 2010

Miyazaki Kanko Hotel, Miyazaki, Japan

Thursday Morning -March 4, 2010 AJCPP2010 in Miyazaki

Thursday Morning -March 4, 2010

Session Room C2nd Floor “Hatsukari”

Session Room D2nd Floor “Oniji”2nd Floor Hatsukari 2nd Floor Oniji

Time C1. Pre-cooled Turbo Engine 1 Sadatake Tomioka (JAXA)

Jai-ick Yoh (Seoul National University)

D1. Engine System

HisaoFutamura (JAXA)Hwanil Huh (Chungnam National University)

0820

0840 [AJCPP2010-053]Qualification Test of a Hypersonic Turbojet Engine for a Flight ExperimentHideyuki Taguchi, Kenya Harada, Hiroaki Kobayashi, Takayuki Kojima, Motoyuki Hongoh,Daisaku Masaki, Shujiro Sawai, Yusuke Maru (JAXA), Tetsuya Sato (Waseda University)

[AJCPP2010-072]Consideration of Intercooled and Recuperated Jet Engine Using Super-critical CO2Yutaka Ito, Takao Nagasaki (Tokyo Institute of Technology)

0900 [AJCPP2010 143] [AJCPP2010 112]0900 [AJCPP2010-143]Windmilling Start of the Precooled Turbojet Engine during Supersonic FlightHiroaki Kobayashi, Hideyuki Taguchi, Takayuki Kojima, Yusuke Maru, Shujiro Sawai (JAXA)

[AJCPP2010-112]A study on the turbofan cycle with heat exchangersTetsuya Shinmyo, Koji Okamoto, Susumu Teramoto, Toshio Nagashima (University of Tokyo)

0920 [AJCPP2010-137]Performance Tests of a Small Combustion Wind Tunnel for Engine Start Simulation ofHydrogen Turbo Jet at High-altitudesYukihiro Soeta, Hiroshi Nomura (Nihon University), Keiichi Okai (JAXA)

[AJCPP2010-061]Study on GUI Type Gas Turbine Performance Simulation Using Inversely GeneratedComponent Maps and LabVIEWChangduk Kong, Semyeong Lim, Keonwoo Kim (Chosun University)

0940 [AJCPP2010-042]Combustion Characteristic of Pre-Cooled Turbo Jet AfterburnerShunsuke Nishida, Hisashi Taneda (University of Tokyo), Hideyuki Taguchi, Takayuki

[AJCPP2010-162]Off-design performance consideration on tubofan engineHisao Futamura (JAXA)Shunsuke Nishida, Hisashi Taneda (University of Tokyo), Hideyuki Taguchi, Takayuki

Kojima, Motoyuki Hongoh (JAXA), Osamu Imamura, George Ianus, Masafumi Utsumi, TakeoOkunuki (University of Tokyo), Mikiya Araki (Gunma University), Mitsuhiro Tsue (University

Hisao Futamura (JAXA)

1000 [AJCPP2010-123]The Flow Field in Afterburner with Flame-holding Strut for Hypersonic VehicleRyosuke Saito, Akira Kondo, Shoji Sakaue, Takakage Arai (Osaka Prefecture University),Hideyuki Taguchi, Takayosi Kojima, Hiroaki Kobayashi (JAXA)

[AJCPP2010-071]Propulsion System Integration to the Coming 150-seater BWB-like AirlinerMakoto Shibata (JAXA)

1020 [AJCPP2010-050]Dynamic Simulation of Pre-cooled Turbo Jet EngineTomoyuki Arai, Tetsuya Sato (Waseda University), Hideyuki Taguchi, Hiroaki Kobayashi(JAXA)

1040

Break

Keynote Speech 1Toshinori Watanabe (University of Tokyo)


1100 [AJCPP2010-S01]HTV First Mission Results and Future PlanHiroshi Sasaki (JAXA)

Coffee Break

Hiroshi Sasaki (JAXA)


1300Lunch Break

Thursday Afternoon-March 4, 2010 AJCPP2010 in Miyazaki



Time A2.Numerical Simulation for Liquid Rocket Propulsion 2 Nobuhiro Yamanishi (JAXA)

B2. Aircraft Engine Test

Hiroaki Kobayashi (JAXA)

1300 [AJCPP2010-140]A Theoretical and Numerical Investigation for LOx Mixing in a Swirl Injector at SupercriticalConditionsKuk-Jin Kim, Jun-Young Heo, Jong-Chan Kim, Hong-Gye Sung (Korea Aerospace University),Vi Y (G i I tit t f T h l )

[AJCPP2010-097]Evaluation testing for Aero-Propulsion Controls and Accessories systemsYoshiki Miyairi, Masayuki Maniwa, Masashi Shinomiya, Tomonori Oyobe (Japan Ministry ofDefense)

Vigor Yang (Georgia Institute of Technology)

1320 [AJCPP2010-147]Liquid Jet Dynamics and Atomization Characteristics at Near-Field of Coaxial Type InjectorChihiro Inoue, Toshinori Watanabe, Takehiro Himeno, Seiji Uzawa (University of Tokyo)

[AJCPP2010-113]Development Status of a Turbo-Shaft Engine for Korean Utility HelicopterJae Hwan Kim, Iee Ki Ahn, Dae Sung Lee (Korea Aerospace Research Institute), Ok SuckSung, Seung Bae Chen (Samsung Techwin)

1340 [AJCPP2010-095]Numerical Study of the Injection of Liquid Nitrogen at Supercritical ConditionSeong-Young Moon, Jae-Ryul Shin, Jeong-Yeol Choi (Pusan National University)

1400 [AJCPP2010-081]A Numerical Study on a Turbulent Mixing Layer under Transcritical ConditionsHiroumi Tani, Susumu Teramoto, Toshio Nagashima (University of Tokyo)

[AJCPP2010-052]CFD Analysis of Pressure Recovery in Supersonic Diffuser of a High Altitude EnvironmentalTest FacilityGeorge.O.Omollo, Kong ChangDuk (Chosun University), Choe KyoungHu (Atics Eng.)

1420 [AJCPP2010-011]1420Analysis of Performance Parameters and Emissions of Jet Engine During ClimbEnis T. Turgut (Anadolu University)

1440

A3.Nozzle and AerodynamicsTakeo Tomita (JAXA)

B3. Axial Flow Turbine and Compressor 2

Osamu Nozaki (JAXA)

Coffee Break

Takeo Tomita (JAXA)Woong-sup Yoon (Yonsei University)

Osamu Nozaki (JAXA)Soo Seok Yang (KARI)

1500 [AJCPP2010-066]Numerical Analysis of Secondary Injection from Multihole for Thrust Vector Control onSupersonic NozzleHye-jin Lee, Sang-min Kim, Woong-sup Yoon (Yonsei University)

[AJCPP2010-158]Numerical Study on Unsteady Aerodynamic Characteristics of Oscillating Cascades with TipClearanceTaro Tokai, Toshinori Watanabe, Takehiro Himeno, Seiji Uzawa (University of Tokyo)

1520 [AJCPP2010-067]Experiments on the supersonic nozzle plume perturbed by the Secondary Injection jetsJi-Hoon Kang, Tae-Ho Ko, Hyung-Min Kim, Woong-Sup Yoon (University of Yonsei)

[AJCPP2010-078]Dynamic pressure measurement on the rotating blade suction surface of an axialcompressorWang Qingwei, Liu Bo, Xiang Xiaorong, Bo Xiangfeng, Hou Weimin (Northwestern

1540 [AJCPP2010-039]Unsteady Flow Characteristics and Lateral Forces in an Over Expanded Rocket Nozzle

S ( )

[AJCPP2010-012]Experimental Research on Boundary Layer on Compressor Cascade Blade Surface

f ( )Vincent Lijo, Jong-Sung Lee, Huey Dong Kim (Andong National University), ToshiakiSetoguchi, Shigeru Matsuo (Saga University)

Liu-bo, Bo Xiang-feng (Northwestern Polytechnical University)

1600 [AJCPP2010-043]An Investigation of Flow Fluctuation in Overexpanded Dual-Bell NozzleDzianis Proshchanka, Koichi Yonezawa, Hidekazu Koga (Osaka University), KazuhikoYokota (Nagoya Institute of Technology), Tatsuya Kimura, Kenichi Niu (MHI Ltd., NagoyaGuidance & Propulsion Systems Works), Yoshinobu Tsujimoto (Osaka University)

[AJCPP2010-076]Experimental and Numerical Investigation of Stator Wake Flow Characteristic in SingleStage Axial-CompressorXiang Xiaorong, Liu Bo, Liang Jun, Wang QingWei (Northwestern Polytechnical University)

1620 [AJCPP2010-075]Experimental Study on Sound Pressure Characteristics of Rocket Nozzle in IndoorJuHyuong Yoo, HoukSeop Han (Hanwha Corporation)

[AJCPP2010-127]Design and Performance Assessment of Multi Stage Axial CompressorYoung-Seok Kang, Tae-Choon Park, Soo-Seok Yang (Korea Aerospace Research Institute)

1640 [AJCPP2010-065]Effect of turbulence models on Unsteady Separated Flow in a Rocket NozzleSeiji Tsutsumi, Taro Shimizu, Ryoji Takaki, Takeo Tomita (JAXA)

1700 [AJCPP2010-164]A Research of Discontinuous Galerkin Method Based on Different Numerical FluxesX.D. Ren, F. Feng, C.W. Gu (Tsinghua University)

[AJCPP2010-006]The Effects of Fouling and Erosion on Performance Characteristics Curve of CompressorsAmir Kh. Nezami, Hiwa Khaledi (MPG Company)

HTV first mission (Credit: NASA/JAXA)HTV first mission (Credit: NASA/JAXA)

Thursday Afternoon-March 4, 2010 AJCPP2010 in Miyazaki


Session Room D2nd Floor “Oniji”

Time C2. Hybrid Rocket

Toru Shimada (JAXA)

D2.Miscellaneous Electric Propulsion Satoshi Hosoda (JAXA)

1300 [AJCPP2010-131]Evaluation of C* Efficiency of Swirling-Oxidizer-Flow-Type Hybrid Rocket EngineYuasa Saburo, Sakamoto Masafumi (Tokyo Metropolitan University), Shiraishi Noriko(JAXA), Sezaki Chinatsu, Ide Tatsuya, Masugi Miho, Sakurai Takashi (Tokyo MetropolitanU i it )

[AJCPP2010-136]Micro-thruster Options for the Japanese Space Gravitational Wave Observatory MissionsIkkoh Funaki (JAXA), Yoshinori Nakayama (National Defense Academy), Hideyuki Horisawa(Tokai University)

University)

1320 [AJCPP2010-079]Effects of Flow Swirl on Heat-Transfer of Hybrid Rocket GrainRiichi Itakura, Koji Okamoto, Susumu Teramoto, Toshio Nagashima (University of Tokyo)

[AJCPP2010-009]A Cost Evaluation for Transport of Solar Power Satellite by Beam Energy PropulsionKohei Shimamura, Hironori Sawahara, Akinori Oda, Kimiya Komurasaki, Yoshihiro Arakawa(University of Tokyo)

1340 [AJCPP2010-013]Regression Rate Characteristics and Combustion Mechanism of Some Hybrid Rocket FuelsSatoshi HIKONE, Takao HASAEGAWA, Ichiro NAKAGAWA (Tokai University)

[AJCPP2010-033]Development and Ground Test of an HTP Arcjet SystemHou-Yi Lee, Yueh-Heng Li, Guan-Bang Chen, Yei-Chin Chao (National Cheng Kung University)

1400 [AJCPP2010-018]Design and Development of a Laboratory Benchmark Pulsed Plasma Thruster for the FirstTime in West AsiaAbdolrahim Rezaeiha, Mehdi Anbarloui, Mohammad Farshchi (Sharif University of

1420 [AJCPP2010-134] [AJCPP2010-014]1420The Development and Test of the N2O Oxidizer in large-scale Hybrid RocketMeng Chun Hsu, Hung Wei Hsu, Tsung Sheng Lee, Tang An Jhan (National Cheng KungUniversity)

Modeling for the Energy Absorption Rate Prediction of Thin-walled Cells with Square andCircular Cross-sections Employing GMDH-type Neural Network and Genetic AlgorithmAmir Maravandi (Isalamic Azad University, Majlesi Branch)

1440

C3. Pre-cooled Turbo Engine 2

Kouichiro Tani (JAXA)

D3. Hall Thruster

Ikkoh Funaki (JAXA)

Coffee Break

Kouichiro Tani (JAXA)Guang Xi (Xi’an Jiaotong University)

Ikkoh Funaki (JAXA)

1500 [AJCPP2010-045]Estimation of a Temperature Distortion Effect on the Small Pre-Cooled Turbojet EngineCompressorKenichiro Maruyama (Tokyo University of Science), Hideyuki Taguchi, Daisaku Masaki,Kenya Harada, Hiroaki Kobayashi (JAXA), Shinji Honami (Tokyo University of Science)

[AJCPP2010-085]Improvement of Erosion Rate Measurement Using Multilayer Coated ChipShinatora Cho, Shigeru Yokota, Kentaro Hara, Daisuke Takahashi, Yoshihiro Arakawa,Kimiya Komurasaki (University of Tokyo), Akira Kobayashi (Osaka University)

1520 [AJCPP2010-073]Numerical Investigation on the Intake Performance of the Hypersonic TurbojetExperimental AircraftTanabe, A., Matsuo, A. (Keio University), Kojima, T., Taguchi, H. (JAXA)

[AJCPP2010-122]Erosion Measurement of a Hall Thruster Using Optical Emission SpectroscopyShigeru Yokota, Ryotaro Kaneko, Shinatora Cho, Kentaro Hara, Daisuke Takahashi, KimiyaKomurasaki, Yoshihiro Arakawa (University of Tokyo)

1540 [AJCPP2010-027]An Experimental Study on Inlet Buzz Characteristics

S (

[AJCPP2010-047]Observations of low frequency oscillation current and control method in 20mN-class Hall

Tomohiro Nakayama, Keita Miyamura, Masahiro Akatsuka, Tetsuya Sato (WasedaUniversity), Takayuki Kojima, Hideyuki Taguchi (JAXA)

thrusterHiroyuki Osuga (Mitsubishi Electronic/Nagasaki University), Fujio Kurokawa (NagasakiUniversity), Taichiro Tamida (Mitsubishi Electronic), Naoji Yamamoto, Ezaki Toru (KyushuUniversity)

1600 [AJCPP2010-156]Numerical Analysis of Heat Transfer and Fluid Flow around Heat Exchangers for AirBreathing EngineMakoto Terada, Toshinori Watanabe, Takehiro Himeno (University of Tokyo)

[AJCPP2010-049]Development of a low power Hall thrusterNaoji Yamamoto, Toru Ezaki, Hideki Nakashima (Kyushu University)

1620 [AJCPP2010-103]Fuel Supply System of Precooled Turbojet Engine and Flight Experiment VehicleTakayuki Kojima, Hideyuki Taguchi, Hiroaki Kobayashi, Kenya Harada, Motoyuki Hongoh,Shujiro Sawai, Yusuke Maru (JAXA), Tetsuya Sato (Waseda University)j , ( ), y ( y)

1640 [AJCPP2010-077]Temperature Measurement of Supersonic Exhaust Gas from Hypersonic Turbojet EngineShuhei Takahashi, Hirotaka Wada, Kazunori Wakai (Gifu University), Shunsuke Nishida,Osamu Imamura, Mitsuhiro Tsue (University of Tokyo), Hideyuki Taguchi, Takayuki Kojima(JAXA)

1700

www.jsass.or.jp/propcom/ajcpp2010

Friday Morning -March 5, 2010 AJCPP2010 in Miyazaki



Time A4. Radial Turbomachinery

Liu Bo (Northwestern Polytechnical University)Susumu Teramoto (University of Tokyo)

B4. Combustor

Seongman Choi (Chonbuk National University)Mitsuhiro Tsue (University of Tokyo)

0800 [AJCPP2010-157]Numerical Analysis of Super-critical Carbon-dioxide Flows in a Centrifugal CompressorTakayuki Tan, Takehiro Himeno, Toshinori Watanabe (University of Tokyo), MotoakiUt (T k I tit t f T h l ) Hi hi H ik (Th I tit t f A li d E )

[AJCPP2010-125]Combustion Characteristics and Practical-use Issues of Engineering-Model of Hydrogen-Fueled Ultra-micro Combustor for UMGTF d T k hi S k i T k hi Y S b (T k M t lit U i it )Utamura (Tokyo Institute of Technology), Hiroshi Hasuike (The Institute of Applied Energy) Fueda Takeshi, Sakurai Takashi, Yuasa Saburo (Tokyo Metropolitan University)

0820 [AJCPP2010-086]Experimental Study on Heat Exchanger (HEX)-Combustor For Ultra Micro Gas TurbineTurkeli Ramadan Zerrin, Yamaguchi Kazuo, Okamoto Koji (University of Tokyo), SakuraiTakashi (Tokyo Metropolitan University)

0840 [AJCPP2010-080]Numerical Investigation of Inlet Effects on Tesla Turbine PerformanceTakafumi Hidema, Koji Okamoto, Susumu Teramoto, Toshio Nagashima (University ofTokyo)

[AJCPP2010-107]Performance tests of the slinger combustor for a micro turbo-jet enginePoomin Park, Hyungmo Kim, Sooseok Yang (Korea Aerospace Research Inst.), Donghun Lee(Samsung Techwin, Power System R&D Center), Gyungwon You (Agency for DefenseDevelopment)

0900 [AJCPP2010-032]Performance Characterization of a Millimeter-Scale Centrifugal ImpellerYan Ma, Guang Xi (Xi’an Jiaotong University)

[AJCPP2010-092]Enhancement of Methane Combustion in Micro Channels: Effects of Catalyst Segmentationwith CavitiesYueh-Heng Li, Guan-Bang Chen, Hung-Wei Hsu, Hou-Yi Lee, Yei-Chin Chao (National ChengKung University)

0920 [AJCPP2010-030]Performance Improvement of a Low Flow Coefficient Centrifugal Compressor Impellerthrough Optimization DesignZhiheng Wang, Guang Xi (Xi’an Jiaotong University)

[AJCPP2010-035]An Experimental Study of the Rotating Fuel Injector for the Micro Turbojet ApplicationSeong Ho Jang, Seong Man Choi (Chonbuk National University)

0940 [AJCPP2010-055]Design and Flow Field Analysis on Vaned Diffuser in Centrifugal CompressorCui Wei-wei, Du Jian-yi, Xu Jian-zhong (Chinese Academy of Science)

[AJCPP2010-120]Air Flow Control on High Pressure Combustion Test by Fluidic Diverter for Air Blast FuelNozzleSeiji Yoshida, Takeshi Yamamoto, Yoji Kurosawa, Kazuo Shimodaira (JAXA)

1000

A5.Numerical Simulation for Liquid Rocket Propulsion 3Yutaka Ito (Tokyo Institute of Technology)

B5. Engine Noise Reduction

Mitsumasa Makida (JAXA)

1020 [AJCPP2010-145]Numerical Analysis of Control of Cavitation Instabilities in Tandem CascadeYuka Iga (Tohoku University), Yoshiki Yoshida (Tohoku University/JAXA)

[AJCPP2010-126]High-Subsonic Hot Jet Noise Measurements for Millimeter-Sized NozzlesYuta Nakanishi, Koji Okamoto, Susumu Teramoto, Toshio Nagashima (University of Tokyo)

1040 [AJCPP2010-161] [AJCPP2010-090]

Coffee Break

1040 [ ]Numerical Study on Cavitating Flow in Two-dimensional HydrofoilTakafumi Kudo, Toshinori Watanabe, Takehiro Himeno (University of Tokyo)

[ ]Study for Short Ejector PerformanceJu Hyun Im, Seung Jin Song (Seoul National University)

1100 [AJCPP2010-160]Numerical analysis of free-surface flows coupled with heat transfer and phase change inspace transportation systemsYutaka Umemura, Takehiro Himeno, Toshinori Watanabe, Seiji Uzawa (University of Tokyo)

[AJCPP2010-057]Active Control Experiments for Fan NoiseTakeshi Nakagawa, Nobuhiko Yamasaki (Kyushu University)

1120 [AJCPP2010-064]A Numerical Investigation of Cryogenic Cavitation Inception with a Noncondensable GasShin-ichi Tsuda (JAXA), Mitsuo Koshi (University of Tokyo), Nobuhiro Yamanishi (JAXA),Yoichiro Matsumoto (University of Tokyo)

[AJCPP2010-034]Fan Noise Prediction for Rotor/Stator Acoustic Interaction in Fan DuctS. Kusuda, H. Kodama, T. Ooishi, N. Tsuchiya (IHI Corporation), M. Namba

1140 [AJCPP2010-152] [AJCPP2010-155]1140 [AJCPP2010-152]Numerical Study on the Deformation of an Oxygen Droplet in a Hydrogen Stream at HighPressuresKazuya Shimizu, Mituso Koshi (University of Tokyo)

[AJCPP2010-155]Experimental and Numerical Study of Microjet Injection for Supersonic Jet Noise ReductionRyuichi Okada, Toshinori Watanabe, Seiji Uzawa, Takehiro Himeno (University of Tokyo),Tsutomu Oishi (IHI Corporation)


Lunch Break1300

Lunch Break

Friday Morning -March 5, 2010 AJCPP2010 in Miyazaki



Time C4.Solid Rocket MotorJeong Soo Kim (Pukyong National University)

D4.SCRAM Jet Engine 1Yung Hwan Byun (Konkuk University) Tetsuya Sato (Waseda University)

0800 [AJCPP2010-087]Ramjet Mode Experiments of a Rocket-Ramjet Combined-Cycle Engine in Mach 6 FlightConditionsK i K t S H T t Hi i F i i O M T k hi (JAXA)Kanenori Kato, Susumu Hasegawa, Tetsuo Hiraiwa, Fumiei Ono, Masao Takegoshi (JAXA)

0820 [AJCPP2010-083]Numerical Analysis of a Rocket-Ramjet Combined Cycle Engine in Mach 6 Flight ConditionsMasatoshi Kodera, Kouichiro Tani, Shuichi Ueda (JAXA)

0840 [AJCPP2010-099]Operation Characteristics of Pyrogen Type Ignitor from the Motor Case Strain DataTaeho Rho, Kwontae Hoon (HANWHA Corporation), In-Hyun Cho (Korea Aerospace ResearchInstitute)

[AJCPP2010-119]Introduction of Supersonic Hot Streak Ignition for SCRAM Jet EngineShigeo Obata, Manabu Tagashira, Yousuke Ura, Takuhiko Yatabe (National DefenseAcademy)

0900 [AJCPP2010-100]Cookoff simulation of solid rocket motorKi-hong Kim, Tae-yong Jung, Kyung-cheol Lee (Seoul National University), Young-dae Doh,

[AJCPP2010-037]Development of Ignition Enhance method by Using Non-equilibrium Plasma in High SpeedFlow

Ji-chang Yoo (Agency for Defense Development), Jai-ick Yoh (Seoul National University) Takamasa Yamamoto, Yoshinori Matsubara, Kenichi Takita, Toshinori Kouchi (TohokuUniversity)

0920 [AJCPP2010-101]Simulation of structural damage caused by the gaseous deflagration-to-detonationtransitionMin-cheol Gwak, Jai-ick Yoh (Seoul National University)

[AJCPP2010-022]Ignition Characteristics of Plasma Jet Using Ar-based Mixed Feedstock in Supersonic FlowPierre-Edouard A.A. Bossard, Kentaro Kurumada, Yoshinori Matsubara, Kenichi Takita(Tohoku University)

0940 [AJCPP2010-062]A Study on Size Optimization Design for Rocket Motor Case with Torispherical Dome TypeYoung-Gui Choi, Kwang-Bok Shin (Hanbat National University), Won-Hoon Kim (Agency forDefense Development)

[AJCPP2010-102]Ground test results analysis of the model scramjet engine and componentsYang Ji Lee, Sang Hun Kang, Soo Seok Yang (Korea Aerospace Research Institute)

Break

1000

C5. Numerical Simulation for Solid/Hybrid Rocket Propulsion

Taro Shimizu (JAXA)

D5. Space Transportation Projects

Hiroshi Aoki (JAXA)

1020 [AJCPP2010-041]LES of Turbulent Flow in Planar Channel Imposed with Wall BlowingYang Na, Changjin Lee (Konkuk University)

[AJCPP2010-074]Safety Program for KSLV-I, NaroSang Yeon Cho, Myung Ho Shin, Seung Hyub Oh, Gwang Rae Cho (Korea AerospaceResearch Institute)

1040 [AJCPP2010-028] [AJCPP2010-154]

Coffee Break

1040 [ ]Unsteady Internal Ballistics of Hybrid Rocket: Quasi-1D SimulationYuki Funami (University of Tokyo), Vasily Novozhilov (University of Ulster), Toru Shimada(JAXA)

[ ]Development Status of LNG Engine (LE-8)Hiroaki Sakai, Yoshihiro Torii (JAXA), Yoshinobu Yasutomi, Masahiro Ishii (IHI AerospaceCo., Ltd.)

1100 [AJCPP2010-141]Unified software development for solid rocket propulsion system designKyoungHoon Kang, JunHo Lee, Hyuk Suh (Hanwha Corp., Ltd.)

[AJCPP2010-116]Development of L-605 Nozzle ExtensionTakayuki Motogi, Manabu Moteki, Taiga Yoshida, Isao Tate (IHI Aerospace Co., Ltd.),Kiyoshi Kinefuchi, Toru Kamita, Yoshihiro Torii (JAXA)

1120 [AJCPP2010-088]Numerical Simulation on Unsteady Compressible Low-Speed Flow Using PreconditioningMethod: Comparison between AUSMDV and AUSM+-upNobuyuki Tsuboi (Kyushu Institute of Technology), Katsuyoshi Fukiba (Muroran Institute ofTechnology), Toru Shimada (JAXA)

[AJCPP2010-118]Experimental Investigation and Numerical Approach of Liquid propellant residual in RocketTank BottomMasanobu Fujimura, Keisuke Yamada (IHI AEROSPACE Co., Ltd.), Kiyoshi Kinefuchi, ToruKamita (JAXA)

1140 [AJCPP2010-117] [AJCPP2010-056]1140 [AJCPP2010-117]Advanced Computer Science on Internal Ballistics of Solid Rocket Motors: 2009 ProgressReportToru Shimada (JAXA), Kazushige Kato (NOF Corporation), Nobuhiro Sekino (IHI AerospaceCo. Ltd.), Nobuyuki Tsuboi (Kyushu Institute of Technology), Hiroshi Hasegawa (NOFCorporation), Mihoko Fukunaga (IHI Aerospace Co. Ltd.), Yu Daimon (JAXA), HiroyaAsakawa (IHI Aerospace Co. Ltd.)

[AJCPP2010-056]The Performance Evaluation of HTV Propulsion System based on its First FlightShinichi Takata, Tsutomu Fukatsu, Takane Imada (JAXA)


Lunch Break1300

Lunch Break


Friday Afternoon-March 5, 2010 AJCPP2010 in Miyazaki



Time A6.Liquid Rocket Propulsion System and Ground TestHeuy Dong Kim (Andong National University) Shinichi Takata (JAXA)

B6. Combustion Phenomena

Keiichi Okai (JAXA)Jeong Park (Pukyong National University)

1300 [AJCPP2010-069]A preliminary design study of rotor system for LE-X turbopumpMasaharu Uchiumi, Makoto Kojima, Koichi Okita (JAXA), Tsutomu Mizuno (IHI)

[AJCPP2010-036]Flame Visualization of the Annular Reverse Sector CombustorBorami Kim (Chonbuk National University), Cheahong Choi, Dongho Rhee (Korea AerospaceR h I tit t ) S Ch i (Ch b k N ti l U i it )Research Institute), Seongman Choi (Chonbuk National University)

1320 [AJCPP2010-021]Advanced Stability Analysis of Propulsion System for Future Launch VehiclesShusuke Hori (JAXA)

[AJCPP2010-023]An Experimental Study of Combustion Instability Characteristics in Model Dump ShapeCombustor by Reproduction of GE 7FA+e DLN-2.6Sungsoon Park, Min-Ki Kim, Jang-Su Lee, Youngbin Yoon (Seoul National University)

1340 [AJCPP2010-054]Design and Performance Evaluation of a Flow Regulator for the Thrust Control of a LiquidRocket EngineTaekyu Jung, Sooyong Lee (Korea Aerospace Research Institute)

[AJCPP2010-048]A Semi-Active Control of the Combustion Instability in a Ducted Premixed FlameJaecheon Song, Jinkwan Song, Jeongjae Hwang, Youngbin Yoon (Seoul NationalUniversity), Jinsoo Cho (Hanyang University)

1400 [AJCPP2010-070]Aerodynamic Characteristics of Butterfly Valves in Transonic Moist Air Flow withHomogeneous CondensationA.B.M. Toufique Hasan, Shigeru Matsuo, Toshiaki Setoguchi (Saga University), Heuy Dong

[AJCPP2010-138]A study on cellular instability in outwardly propagating spherical syngas-air premixedflames diluted with CO2, N2, and HeT.M. Vu, J. Park, J.S. Kim, O.B. Kwon, D.S. Bae (Pukyong National University)

Kim (Andong National University)

1420 [AJCPP2010-038]Performance Control of Supersonic Exhaust Diffuser Using an Orifice SystemVincent Lijo, Abhilash Suryan, Heuy Dong Kim (Andong National University, Korea), ToshiakiSetoguchi (Saga University)

[AJCPP2010-093]Flame-Luminosity Thermophotovoltaic Power SystemYueh-Heng Li (National Cheng Kung University), Chih-Yung Wu (Kao Yuan University), Tang-An Jhan, Yei-Chin Chao (National Cheng Kung University)

1440 [AJCPP2010-163]Flow Characteristics of Liquid Hydrogen Coolant in Throttling Combustion Tests with aSmall Rocket CombustorTakuo Onodera, Mamoru Takahashi, Masaki Sasaki, Masaki Sato, Shuichi Ueda, TakeoTomita (JAXA)

[AJCPP2010-020]Experimental Investigation of Self-ignition of Pressurized Hydrogen Released by the Failureof a Rupture Disk into a TubeHyoung Jin Lee, Sei-Hwan Kim, Yeong Ryeon Kim, In-Seuck Jeung (Seoul NationalUniversity)

1500

B7.Engine Components Chiyuki Nakamata (IHI Corporation)

1520 [AJCPP2010-010]Conjugate Flow and Heat Transfer Analysis of A Film-Cooled Flat PlateZou Xin, Yuan Xin (Tsinghua University)

Coffee Break

1540 [AJCPP2010-026]Experimental Investigation and Numerical Simulation of Rod-airfoil Unsteady FlowJiajian Zhou, Dakai Lin, Junhui Gao, Xiaodong Li (Beihang University)

1600 [AJCPP2010-109]Innovative multi-physics simulation of shock and reacting flowKi-hong Kim (Seoul National University), Chang-moon Myung (Agency for DefenseDevelopment), Jai-ick Yoh (Seoul National University)

1620

Environmental Icing Test of XF7‐10 for QT (Credit: TRDI, MOD)

1640

Keynote Speech 2Dae Sung Lee (Korea Aerospace Research Institute)


1700

Coffee Break

[AJCPP2010-S02]Current Korean Activities on Research and Development of Air-Breathing Propulsion SystemsChangduk Kong (Chosun University)

Environmental Icing Test of XF7‐10 for QT (Credit: TRDI, MOD)

Banquet Banquet Room3rd Floor “Hekisui”

18305000 JPY/PERSON

Environmental Icing Test of XF7‐10 for QT (Credit: TRDI, MOD)Environmental Icing Test of XF7‐10 for QT (Credit: TRDI, MOD)

Liquid Propellants Made in Miyazaki

Friday Afternoon-March 5, 2010 AJCPP2010 in Miyazaki



Time C6. Injector and Thrust Chamber

Hideshi Kagawa (JAXA)Youngbin Yoon (Seoul National University)

D6.SCRAM Jet Engine 2In-Seuck Jeung (Seoul National University)Hideyuki Taguchi (JAXA)

1300 [AJCPP2010-110]Spray Characteristics in Gas-Centered Swirl Coaxial injectorsJae-Hyoung Jeon, Moongeun Hong, Yeoung-Min Han, Soo Yong Lee (Korea AerospaceR h I tit t )

[AJCPP2010-059]Stereoscopic PIV Measurement of Supersonic Injection Flowfield and Its Error AnalysisShohei Uramoto, Shinichiro Tsuru, Toshinori Kouchi, Goro Masuya (Tohoku University)

Research Institute)

1320 [AJCPP2010-132]Effects of Throttling on the Spray Break-up in an Injector of Direct-injection TypeJeong Soo Kim, Jeong Park, Oh Boong Kwon, Dae Seok Bae (Pukyong National University)

[AJCPP2010-106]Effects of Injectant Species on Compressible Turbulent Scalar Mixing StructureYusaku Horikoshi, Koji Abe, Hidemi Takahashi, Toshinori Kouchi, Goro Masuya (TohokuUniversity)

1340 [AJCPP2010-148]A Challenge of Predicting Thermostructural Response of Ablating SiFRP for the CombustionChamber of Liquid Rocket EnginesYoshiki Matsuura, Kenichi Hirai (IHI Aerospace Co., Ltd.)

[AJCPP2010-058]Numerical Simulation of Pulsed Injection into a Supersonic CrossflowK. Sasaya, J. Watanabe, T. Kouchi, G. Masuya (Tohoku University)

1400 [AJCPP2010-130]Study on Injector Design for a 2kN N2O/Ethanol EngineFumio Okuno (The Graduate University for Advanced Studies (SOKENDAI)), TsuyoshiYagishita (JAXA), Yasuhiro Daimoh (IHI Aerospace Engineering), Fuyuko Fukuyoshi,

[AJCPP2010-104]Numerical Investigation on Effects of Pseudo-Shock Wave for Airflow/Jet MixingT. Kobayashi, A. Matsuo (Keio University), S. Tomioka, M. Izumikawa (JAXA)

Shinichiro Tokudome (JAXA)

1420 [AJCPP2010-031]Spray Characteristics of a Gas-centered Swirl Coaxial InjectorJi-Hyuk Im, Seongho Cho, Gujeong Park, Youngbin Yoon (Seoul National University),Vladimir Bazarov (Moscow Aviation Institute)

[AJCPP2010-060]Three-Dimensional Numerical Analysis of HyShot Scramjet Combustor with a TransverseFuel InjectionSu-Hee Won, In-Seuck Jeung (Seoul National University), Jeong-Yeol Choi (Pusan NationalUniversity)

1440 [AJCPP2010-149]Thermal Issues in the Design of Ablative Combustion Chamber of Liquid Rocket EnginesKenichi Hirai, Yoshiki Matsuura (IHI Aerospace Co., Ltd.), Kiyoshi Kinefuchi, Toru Kamita(JAXA)

[AJCPP2010-124]Effect of Incoming Boundary Layer Characteristics on Breakdown of Supersonic StreamwiseVortices for Supersonic MixingHiroki Hayase, Akira Kondo, Shoji Sakaue, Takakage Arai (Osaka Prefecture University)

1500

D7. Electromagnetic Propulsion

Shigeru Yokota (University of Tokyo)

1520 [AJCPP2010-063]Preliminary Study on Electromagnetic Plasma Acceleration for Electrodeless ElectricPropulsionHiroyuki Nishida, Takahiro Nakamura (Tokyo University of Agriculture and Technology),Ikkoh Funaki (JAXA), Shujiro Shinohara, Tohru Hada (Kyushu University), Takao Tanikawa

Coffee Break

Ikkoh Funaki (JAXA), Shujiro Shinohara, Tohru Hada (Kyushu University), Takao Tanikawa(Tokai University)

1540

1600 [AJCPP2010-094]Orbital Altitude Keeping System by Using Electrodynamic TetherAtsushi Nakajima, Hidekazu Masuda, Kenta Okamoto (Shinshu University), Syuhei Miwa,Yoshiki Yamagiwa (Shizuoka University)

1620 [AJCPP2010-135]Plasma Wind Tunnel for Plasma Sail ExperimentsIkkoh Funaki (JAXA), Kazuma Ueno, Yuya Oshio (Graduate University for Advanced

H‐IIB LaunchVehicle (Credit: JAXA)( ), , y ( y

Studies), Hideyuki Horisawa (Tokai University), Hiroshi Yamakawa (Kyoto University)

1640

Keynote Speech 2Dae Sung Lee (Korea Aerospace Research Institute)


1700

Coffee Break

[AJCPP2010-S02]Current Korean Activities on Research and Development of Air-Breathing Propulsion SystemsChangduk Kong (Chosun University)

H‐IIB LaunchVehicle (Credit: JAXA)

Banquet Banquet Room3rd Floor “Hekisui”

18305000 JPY/PERSON

www jsass or jp/propcom/ajcpp2010




Saturday Morning-March 6, 2010 AJCPP2010 in Miyazaki

Time Keynote Speech 3Toshinori Watanabe (University of Tokyo)


0820 [AJCPP2010-S03]Commercial Aviation Propulsion For The 21st CenturyAlan H. Epstein (V.P. Technology and Environment, Pratt and Whitney)

Keynote Speech 4TBD


0910 [AJCPP2010-S04]0910 [ ]Fundamental Studies on Performance Improvement of Scramjet EngineXinyu Chang, Lihong Chen, Lianjie Yue, Xilong Yu, Hongbin Gu(Institute of Mechanics, Chinese Academy of sciences)

1000



A8. Spacecraft PropulsionSinichiro

B8. SCRAM Jet Engine 3

Coffee Break

p pSinichiro Tokudome (JAXA)Poomin Park (KARI)

gObata Shigeo (National Defense Academy, JAPAN) Hong-Gye Sung (Korea Aerospace University)

1020 [AJCPP2010-068]Study on the Catalytic Decomposition of Nitrous Oxide for a Monopropellant ThrusterTaegyu Kim, Sung Ju Yong (Choun University)

[AJCPP2010-096]Numerical Study on the Combustion Characteristics of Hydrogen and Ethylene Fueled Dual-Mode Scramjet CombustorsJinhyeon Noh (Pusan National University), Su-Hee Won (Seoul National University), Jeong-Yeol Choi (Pusan National University), Jong-Ryul Byun, Jin-Sik Lim (Agency for Defense

1040 [AJCPP2010-128]Catalytic decomposition of N2O for a rocket propulsion systemGia-Hong Wei, Hung-Wei Hsu, Guan-Bang Chen, Yei-Chin Chao (National Cheng KungUniversity)

[AJCPP2010-142]Intake Side Wall Effect of a Scramjet Engine with a Cavity Flame-Holder Using a Unified 3DNumerical AnalysisHyo-Won Yeom, Sung-Jin Kim, Hong-Gye Sung (Korea Aerospace University), Sang HunKang, Soo Seok Yang (Korea Aerospace Research Institute)

1100 [AJCPP2010-017] [AJCPP2010-005]1100 [AJCPP2010-017]Compression-deflection test on the propellant seal materialHideshi Kagawa (JAXA), Mitsuharu Kusama (Advanced Engineering Services Co., Ltd.),Tsuyoshi Takami, Toshikazu Hayashi (MHI, Nagasaki)

[AJCPP2010-005]Combustion Studies in a CavityVijaya kumar. R., S.C. Gupta (MVJCE, Bangalore), Vidyadhar.Y. Mudkavi (Scientist ‘F'NAL,Bangalore)

1120 [AJCPP2010-133]Plug Nozzle Scale Model TestIdeo Masuda, Kenichi Kajiwara (JAXA)

[AJCPP2010-003]Conservation-Law Approach to Prediction of Boundary Layer TransitionTakeshi Kanda (JAXA)

1140 [AJCPP2010-046]Design and Flow Analysis of the Two-Dimensional Convergent-Divergent Thrust VectoringNozzleYoonhee Kim, Hanjin Jung, Seongman Choi (Chonbuk National University), Hyunsoo Chang

1200 [AJCPP2010-114]Intake Buzz Margin Control of the Supersonic Propulsion System based on IntegratedDynamic ModelSun-Kyoung Kim, Sung-Jin Kim, Hyo-Won Yeom, Chang-Soo Jeon, Hong-Gye Sung (School ofAerospace and Mechanical Engineering), Ik-Soo Park (Korea Advanced Institute of Scienceand Technology)

Lunch Break

1300 Post-congress Tour Saitobaru Archaelogical Museum andAya Shusen-no-Mori

Tour bus will deaprt at hotel entrance4000 JPY/PERSON

1800

Saitobaru Archelogical Museum Theme Park on Shochu and Wine

Saturday Morning-March 6, 2010 AJCPP2010 in Miyazaki

Time Keynote Speech 3Toshinori Watanabe (University of Tokyo)


0820 [AJCPP2010-S03]Commercial Aviation Propulsion For The 21st CenturyAlan H. Epstein (V.P. Technology and Environment, Pratt and Whitney)

Keynote Speech 4TBD


0910 [AJCPP2010-S04]0910 [ ]Fundamental Studies on Performance Improvement of Scramjet EngineXinyu Chang, Lihong Chen, Lianjie Yue, Xilong Yu, Hongbin Gu(Institute of Mechanics, Chinese Academy of sciences)

1000


C8.Solid/Hybrid Rocket Propellant

Coffee Break

y p Hiroto Habu (JAXA) Tae Seong Roh (Inha University)

1020 [AJCPP2010-144]Numerical Prediction of Microwave-Rocket Plume InteractionKiyoshi Kinefuchi (University of Tokyo), Ikkoh Funaki, Toru Shimada, Takashi Abe (JAXA)

1040 [AJCPP2010-129]Development of low cost fuels for hybrid rocket engineAkiyo Aoki, Apollo B. Fukuchi (IHI AEROSPACE Co., Ltd.)

1100 [AJCPP2010-121]1100 [AJCPP2010-121]Effect of Flame Retardant on the Mechanical and Thermal Properties of EPDM-based RubberJin-Yong Kim, Won-Bok Lee, Hyuk Suh (Hanwha Corporation), Young-Woo Rhee (ChungnamNational University)

1120 [AJCPP2010-115]Nonintrusive Diagnostics of Distribution of AP Particles in Composite PropellantsHiroshi Hasegawa, Kazushige Kato (NOF Corporation), Hideo Miyachi (KGT Inc.), MihokoFukunaga (IHI Aerospace Co., Ltd.), Nobuyuki Tsuboi (Kyushu Institute of Technology),Yuzou Yajima, Katsumi Hiraoka (Tokai University), Yu Daimon (JAXA), Toru Shimada(Institute of Space and Astronautical Science)

1140 [AJCPP2010-029]Three Dimensional Ellipsoidal Random Packing and Their Analysis with Combustion Modelfor Solid Rocket PropellantYuzo Yajima (Tokai University), Toru Shimada (JAXA), Katsumi Hiraoka (Tokai University)

1200 [AJCPP2010-111]Study on Properties of Interior Ballistics According to Solid Propellant Grain Configurationand ArrangementHyung-Gun Sung, Jin-Sung Jang, Dong-Whan Choi, Tae-Seong Roh (Inha University)

Lunch Break

LNG rocket engine (Credit: JAXA)

1300 Post-congress Tour Saitobaru Archaelogical Museum andAya Shusen-no-Mori

Tour bus will deaprt at hotel entrance4000 JPY/PERSON

1800

LNG rocket engine (Credit: JAXA)LNG rocket engine (Credit: JAXA)LNG rocket engine (Credit: JAXA)


March 4 - 6, 2010 Miyazaki Kanko Hotel, Miyazaki-City, Japan

Asian Joint Conference on Propulsion and Power 2010

100 kN thrust class LNG rocket engine

(Credit: JAXA)

Successful lift-off of H-IIB Launch Vehicle

(Credit: JAXA)

HTV just before fi rm grasp by the robotic arm(Credit: NASA/JAXA)

Environmental Icing Test of XF7-10 for QT(Credit: TRDI, MOD)

[Keynote Speeches](1) HTV First Mission Results and Future Plan Mr. Hiroshi Sasaki (Function Manager, HTV project team, JAXA)(2) Current Korean Activities on Research and Development of Air-Breathing Propulsion Systems Dr. Changduk Kong (Professor, Department of Aerospace Engineering, Chosun University)(3) Jet Engine Technology for the 21st Century Dr. Alan Epstein (Vice President, Technology and the Environment Pratt & Whitney)(4) Fundamental Studies on Performance Improvement of Scramjet Engine Dr. Xinyu Zhang (Professor, Institute of Mechanics, Chinese Academy of Sciences)

[Organized Session](1) Numerical Approach for Liquid Rocket Engine Design

[General Sessions](1) Aircraft Engine(2) Rocket Propulsion (Solid / Liquid / Hybrid)(3) Electric Propulsion and Advanced Propulsion(4) Propulsion System for Reusable Launch Vehicles(5) Structural / Material Technology(6) Engine Components / Performance (Turbomachinery / Combustor)(7) Combustion, Diffusion / Turbulent Mixing(8) CFD(9) Measurement Techniques and Control / Ground Test(10) Reliability, Operation and Maintenance(11) Others

[Registration Fee]Regular 15,000 JYStudent 8,000 JY

[Location]Miyazaki Kanko Hotel (Miyazaki-City, Japan)

Organized by The Japan Society for Aeronautical and Space Sciences (JSASS)Co-organized by The Korean Society of Propulsion Engineering (KSPE) The Chinese Society of Engineering Thermophysics (CSET)Collaborated by Gas Turbine Society of Japan (GTSJ) The Japan Society of Mechanical Engineers (JSME) Japan Aeronautical Engineers' Association.

The Japan Society for Aeronautical and Space SciencesHP : http//www.jsass.or.jp/propcom/ajcpp2010/

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asian joint c propulsion and p 2010 - jsass.or.jp€¦ · prof. kazutaka nishiyama jaxa/institute...

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